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Gross Mass: 1,678,300 kg (3,700,000 lb). Empty Mass: 136,100 kg (300,000 lb). Thrust (vac): 27,034.900 kN (6,077,687 lbf). Isp: 263 sec. Burn time: 144 sec. Propellants: Solid. Isp(sl): 238 sec. Diameter: 6.61 m (21.68 ft). Span: 9.26 m (30.38 ft). Length: 38.11 m (125.03 ft). Country: USA. No Engines: 1. Engine: AJ-260X. Status: Study 1967. Boeing Low-Cost Saturn Derivative Study, 1967 (trade study of 260 inch first stages for S-IVB, all delivering 86,000 lb pyld to LEO): Low Cost Booster, Solid Propellant
Used on Launch Vehicles:
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